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The actual anomaly of a planet in an elliptical orbit.
- ‘We need to convert this into the eccentric anomaly, and the formula is cos E = (e + cos n) / (1 + e cos n).’
- ‘We use Keplers eccentric anomaly in order to get explicit equations for the planetary orbits in a solar system.’
- ‘The maximum difference in Eccentric Anomaly (in radians) will equal the eccentricity of the orbit.’
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